Coefficient of Lift Equation with Coefficient of Normal Force Calculator

✖The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions.ⓘ Coefficient of Force [μ]			+10% -10%
✖The Angle of Attack is the angle between the chord line of an airfoil and the oncoming airflow, influencing lift and drag in fluid dynamics.ⓘ Angle of Attack [α]			+10% -10%

✖The Lift Coefficient is a dimensionless number that represents the lift generated by a body in a fluid flow, crucial for understanding aerodynamic performance.ⓘ Coefficient of Lift Equation with Coefficient of Normal Force [C_L]

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Coefficient of Lift Equation with Coefficient of Normal Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Coefficient = Coefficient of Force*cos(Angle of Attack)
C_L = μ*cos(α)
This formula uses 1 Functions, 3 Variables

Functions Used

cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)

Variables Used

Lift Coefficient - The Lift Coefficient is a dimensionless number that represents the lift generated by a body in a fluid flow, crucial for understanding aerodynamic performance.
Coefficient of Force - The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions.
Angle of Attack - (Measured in Radian) - The Angle of Attack is the angle between the chord line of an airfoil and the oncoming airflow, influencing lift and drag in fluid dynamics.

STEP 1: Convert Input(s) to Base Unit

Coefficient of Force: 0.06 --> No Conversion Required
Angle of Attack: 10 Degree --> 0.1745329251994 Radian (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_L = μ*cos(α) --> 0.06*cos(0.1745329251994)

Evaluating ... ...

C_L = 0.0590884651807328

STEP 3: Convert Result to Output's Unit

0.0590884651807328 --> No Conversion Required

FINAL ANSWER

0.0590884651807328 ≈ 0.059088 <-- Lift Coefficient

(Calculation completed in 00.020 seconds)

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Amrita School of Engineering (ASE), Vallikavu

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Coefficient of Lift Equation with Coefficient of Normal Force Formula

LaTeX Go

Lift Coefficient = Coefficient of Force*cos(Angle of Attack)
C_L = μ*cos(α)

What is angle of attack?

In fluid dynamics, angle of attack is the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving

How to Calculate Coefficient of Lift Equation with Coefficient of Normal Force?

Coefficient of Lift Equation with Coefficient of Normal Force calculator uses Lift Coefficient = Coefficient of Force*cos(Angle of Attack) to calculate the Lift Coefficient, Coefficient of Lift Equation with Coefficient of Normal Force formula is defined as a relationship that describes how the lift generated by an object in a fluid is influenced by the normal force and the angle of attack, impacting aerodynamic performance. Lift Coefficient is denoted by C_L symbol.

How to calculate Coefficient of Lift Equation with Coefficient of Normal Force using this online calculator? To use this online calculator for Coefficient of Lift Equation with Coefficient of Normal Force, enter Coefficient of Force (μ) & Angle of Attack (α) and hit the calculate button. Here is how the Coefficient of Lift Equation with Coefficient of Normal Force calculation can be explained with given input values -> 0.059088 = 0.06*cos(0.1745329251994).

FAQ

What is Coefficient of Lift Equation with Coefficient of Normal Force?

Coefficient of Lift Equation with Coefficient of Normal Force formula is defined as a relationship that describes how the lift generated by an object in a fluid is influenced by the normal force and the angle of attack, impacting aerodynamic performance and is represented as C_L = μ*cos(α) or Lift Coefficient = Coefficient of Force*cos(Angle of Attack). The Coefficient of Force is a dimensionless value that characterizes the relationship between force and flow in Newtonian fluids under hypersonic conditions & The Angle of Attack is the angle between the chord line of an airfoil and the oncoming airflow, influencing lift and drag in fluid dynamics.

How to calculate Coefficient of Lift Equation with Coefficient of Normal Force?

Coefficient of Lift Equation with Coefficient of Normal Force formula is defined as a relationship that describes how the lift generated by an object in a fluid is influenced by the normal force and the angle of attack, impacting aerodynamic performance is calculated using Lift Coefficient = Coefficient of Force*cos(Angle of Attack). To calculate Coefficient of Lift Equation with Coefficient of Normal Force, you need Coefficient of Force (μ) & Angle of Attack (α). With our tool, you need to enter the respective value for Coefficient of Force & Angle of Attack and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Lift Coefficient?

In this formula, Lift Coefficient uses Coefficient of Force & Angle of Attack. We can use 1 other way(s) to calculate the same, which is/are as follows -

Lift Coefficient = 2*(sin(Angle of Attack))^2*cos(Angle of Attack)

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